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SECTION 4 / MAINTENANCE - GUARANTEES 

 
 

Maintenance 

 
Caution: the two outer sections of the leading edge are not identical. They must be attached to their 
correct leading edge tube. If they are reversed it will modify the angle of the washout tubes (“dive 
sticks”), possibly making the wing uncontrollable. 

 
Transport: 

 one of the principal causes of wear on the wings is vehicle transport. To minimize this 

risk, use the provided protective padding during the disassembly and folding of the wing, use a 
ladder (or similar) sufficiently padded, and avoid having the wing overhang the ends. 
 

Maintenance: 

cleaning is done with mild soap and water.  

• 

Regularly wash the wing in fresh water if you fly at the seaside. In this case the frequency 
of the periodic maintenance must be increased. 

• 

In tropical regions, it can be useful to clean with a liquid fungicide.  

After cleaning, the wing must be allowed to dry. It MUST NEVER placed in its cover when it 
is wet. 

• 

Glue spots, of an old registration marking, for example, can be effectively removed by using 
a rag soaked in trichloroethylene.   

 

Storage: 

in a dry dark area, or safe from the light (heat and UV), after making sure that the the 

wing is completely dry. 
 

Ageing:

 exposure to ultraviolet radiation emitted by the sun and reflected by the moon, cause the 

ageing of the fabric and the seams. As far as possible, park your aircraft under shelter, out of the 
sun, between flights.  
Four upper-surface fabric samples, composed of two fabric parts joined by a seam, are stitched 
into the trailing edge, on both sides of the center of the wing. These bands can be cut out, if 
necessary, during periodic maintenance in order to carry out resistance tests. 
 

Periodic Checks: 

 
Every 50 hours you must visually check: 

• 

The luff lines, the mast attachment hook and the trailing edge connections 

• 

All wing cables, the stainless swages and hearts 

• 

The nose plates  

• 

The upper-surface and keel-pocket (center of the wing) seams  

• 

All articulation and attaching bolts 

• 

The batten shock cord 

• 

The tension (very firm) of the outboard battens  

 

After any violent or « heavy » landing,  it is imperative that you check: 

• 

The nose plates 

• 

the straightness of the leading edges (a disassembly is necessary) 

• 

The straightness of the keel 

• 

The straightness of the control frame riser tubes 

• 

The straightness of the control bar,  

• 

The straightness of the cross spars 

• 

The profile of the battens (between right side and left side) 

• 

The nuts and bolts 

• 

The absence of any deformation thimble hearts of all the cables 

• 

The seams of the sail, in particular at the center of the wing 

• 

The hang assembly 

 
 

MAUT – EN DYN 450 

Edition : June 2005 

Section : 4 - 01 

Summary of Contents for DYNAMIC 450

Page 1: ...WING INSTRUCTION AND MAINTENANCE MANUAL DYNAMIC 450 MAUT EN DYN 450 Edition June 2005 Copyright DTA DTA ULM AU Wing n Model Year...

Page 2: ...DTA improves its production constantly and reserves the right to modify the specification the drawing the characteristics the model and or the equipment in the interests of Quality Assurance without i...

Page 3: ...Diagram 2 01 2 02 2 03 JUNE 05 SECTION 3 USE Wing Assembly Disassembly Wing Photographs assembly disassembly Hang Bracket Position Washout Tension Dissymmetry Vibrations Modifications PREFLIGHT Wing...

Page 4: ...he aircraft or to add elements by modifying the estimate of weight will check that the identification registration card is valid and that the identification markings a minimal height of 50 cm for Fran...

Page 5: ...in fast flight and 30 cm from the front strut in slow flight in hang bracket position n 2 CF section 3 03 Note The person s who choose s to use a non DTA airframe will assume ALL the responsibilities...

Page 6: ...3 Plan Views MAUT EN DYN 450 Edition June 2005 Section 1 03...

Page 7: ...g cables Control frame Cross spar left Inner leading edge LEFT Lower side cable Upper side cable Lower rear cables Cross spar cable tensioning lever Keel Outer leading edge sleeve LEFT Washout tube Fr...

Page 8: ...h 110 km h Horizontal maximum speed VH 115 km h 126 km h 138 km h 130 km h 138 km h Landing distance 70 m 70 m 70 m 70 m 70 m Landing distance from 15 m 190 m 190 m 190 m 190 m 190 m Minimum rate of...

Page 9: ...h 110 km h 110 km h 110 km h Horizontal maximum speed VH 126 km h 138 km h 130 km h 138 km h Landing distance 75 m 75 m 75 m 75 m Landing distance from 15 m 195 m 195 m 195 m 195 m Minimum rate of fal...

Page 10: ...LM is NOT designed for Aerobatic flight Inverted flight is completely prohibited Beyond these limits Bank 60 pitch 45 the loss of stability or of control structural failure or tumbling could occur Koc...

Page 11: ...the wing a little dihedral lock the tension lever or goose neck using the pit pin 2 Note the end of the tension lever is divided lock it immediately On the level of the king post the left tensioning...

Page 12: ...1 2 3 4 5 6 7 8 9 10 MAUT DYN 450 Edition June 2005 Section 3 02...

Page 13: ...y close to the wing s stall speed Control deflections must be subtle The effort required to pull the control bar in will be more significant than in hang position n 2 At MTOW in position n 4 full fron...

Page 14: ...ord on this side Vibration the appearance at high speed of a vibration of the wing trailing edges is a result of insufficient tension on the shock cord of the battens where the vibration occurs Modifi...

Page 15: ...ashout tube dive stick is correctly inserted in the leading edge tube then immediately close the hatch again Walking towards the keel and visually check the batten position and the shock cord 5 Open t...

Page 16: ...ack towards the pilot in order to preserve a trajectory parallel with the runway Let the Microlight ULM accelerate up to 80 km h before climbing out The climb out airspeed should not be lower than 75...

Page 17: ...face disturbs the air flow The stall angle of the wing will be decreased The associated stall speed will increase by approximately 10 km h If you wipe the leading edges before the flight wipe both sid...

Page 18: ...traviolet radiation emitted by the sun and reflected by the moon cause the ageing of the fabric and the seams As far as possible park your aircraft under shelter out of the sun between flights Four up...

Page 19: ...onditions of use of the aircraft given to the purchaser The breaking of any regulatory provisions of the Civil Aviation Code or any related legislation of the country of registration of the aircraft h...

Page 20: ...ASTIC CENTERING RING KEEL E2195 RIGHT LEADING EDGE REAR SECTION 450 E7177 CHC 6X80 12 CONTROL FRAME CHANNEL KEEL E2196 LEFT LEADING EDGE REAR SECTION 450 E7178 CHC 6X37 8 CONTROL FRAME SIDE UPPER KNUC...

Page 21: ...Maintenance Log Date Hours Operations carried out Sign MAUT DYN 450 Edition June 2005 Section 5 02...

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